This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.

本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。

youdao

This paper introduces the parameter estimation research for the turbine inlet temperature and compressor exit pressure by using the engine variables measured under the different flight conditions.

本文研究利用不同飞行状态下测量的发动机变量估计涡轮进口温度和压气机出口压力。

youdao